为分析内冷油腔对活塞的降温效果,对振荡冷却活塞在热负荷、机械负荷及热机耦合作用下的温度场及应力应变分布规律进行研究。采用VOF(volume of fluid)多相流模型、动网格技术等对活塞内冷油腔内机油的振荡传热过程进行Fluent数值模拟,...为分析内冷油腔对活塞的降温效果,对振荡冷却活塞在热负荷、机械负荷及热机耦合作用下的温度场及应力应变分布规律进行研究。采用VOF(volume of fluid)多相流模型、动网格技术等对活塞内冷油腔内机油的振荡传热过程进行Fluent数值模拟,得到内冷油腔各壁面换热系数;将结果映射到活塞固体表面,对活塞分别加载热负荷、机械负荷以及热机耦合作用,对比分析活塞在内冷油腔冷却前后的温度场变化,得到其热应力、机械应力以及耦合应力的变化规律。结果表明,采用内冷油腔进行冷却后,活塞各区域温度均有不同程度下降,其中活塞最高温度下降7.5%;活塞受热机耦合作用下的最大应力小于两者单独作用的结果之和;进行油腔振荡冷却后,活塞的热应力和耦合应力也有不同程度降低。所得到的活塞在内冷油腔冷却前后的应力分布规律,可为活塞内冷油腔的优化设计提供理论参考。展开更多
Vortex-acoustic coupling is one of the most important potential sources of combustion instability in solid rocket motors （SRMs）. Based on the Von Karman Institute for Fluid Dynamics （VKI） experimental motor, the i...Vortex-acoustic coupling is one of the most important potential sources of combustion instability in solid rocket motors （SRMs）. Based on the Von Karman Institute for Fluid Dynamics （VKI） experimental motor, the influence of the thermal inhibitor position and temperature on vortex-shedding-driven pressure oscillations is numerically studied via the large eddy simulation （LES） method. The simulation results demonstrate that vortex shedding is a periodic process and its accurate frequency can be numerically obtained. Acoustic modes could be easily excited by vortex shedding. The vortex shedding frequency and second acoustic frequency dominate the pressure oscillation characteristics in the chamber. Thermal inhibitor position and gas temperature have little effect on vortex shedding frequency, but have great impact on pressure oscillation amplitude. Pressure amplitude is much higher when the thermal inhibitor locates at the acoustic velocity anti-nodes. The farther the thermal inhibitor is to the nozzle head, the more vortex energy would be dissipated by the turbulence. Therefore, the vortex shedding amplitude at the second acoustic velocity antinode near 3/4L （L is chamber length） is larger than those of others. Besides, the natural acoustic frequencies increase with the gas temperature. As the vortex shedding frequency departs from the natural acoustic frequency, the vortex-acoustic feedback loop is decoupled. Consequently, both the vortex shedding and acoustic amplitudes decrease rapidly.展开更多
文摘为分析内冷油腔对活塞的降温效果,对振荡冷却活塞在热负荷、机械负荷及热机耦合作用下的温度场及应力应变分布规律进行研究。采用VOF(volume of fluid)多相流模型、动网格技术等对活塞内冷油腔内机油的振荡传热过程进行Fluent数值模拟,得到内冷油腔各壁面换热系数;将结果映射到活塞固体表面,对活塞分别加载热负荷、机械负荷以及热机耦合作用,对比分析活塞在内冷油腔冷却前后的温度场变化,得到其热应力、机械应力以及耦合应力的变化规律。结果表明,采用内冷油腔进行冷却后,活塞各区域温度均有不同程度下降,其中活塞最高温度下降7.5%;活塞受热机耦合作用下的最大应力小于两者单独作用的结果之和;进行油腔振荡冷却后,活塞的热应力和耦合应力也有不同程度降低。所得到的活塞在内冷油腔冷却前后的应力分布规律,可为活塞内冷油腔的优化设计提供理论参考。
基金the National Natural Science Foundation of China (Grant No.51076015)
文摘Vortex-acoustic coupling is one of the most important potential sources of combustion instability in solid rocket motors （SRMs）. Based on the Von Karman Institute for Fluid Dynamics （VKI） experimental motor, the influence of the thermal inhibitor position and temperature on vortex-shedding-driven pressure oscillations is numerically studied via the large eddy simulation （LES） method. The simulation results demonstrate that vortex shedding is a periodic process and its accurate frequency can be numerically obtained. Acoustic modes could be easily excited by vortex shedding. The vortex shedding frequency and second acoustic frequency dominate the pressure oscillation characteristics in the chamber. Thermal inhibitor position and gas temperature have little effect on vortex shedding frequency, but have great impact on pressure oscillation amplitude. Pressure amplitude is much higher when the thermal inhibitor locates at the acoustic velocity anti-nodes. The farther the thermal inhibitor is to the nozzle head, the more vortex energy would be dissipated by the turbulence. Therefore, the vortex shedding amplitude at the second acoustic velocity antinode near 3/4L （L is chamber length） is larger than those of others. Besides, the natural acoustic frequencies increase with the gas temperature. As the vortex shedding frequency departs from the natural acoustic frequency, the vortex-acoustic feedback loop is decoupled. Consequently, both the vortex shedding and acoustic amplitudes decrease rapidly.
